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Fabrication and experimental evaluation of common domes having waffle-like stiffening. part i- program developmentDetermination of minimum weight shape and stiffening configuration for doubly curved shells subjected to external buckling pressures
Document ID
19650012174
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bellifante, R. J. (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Meyer, R. R. (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Date Acquired
August 2, 2013
Publication Date
November 1, 1964
Subject Category
Structural Mechanics
Report/Patent Number
SM-47742, PT. 1
NASA-CR-62257
Report Number: SM-47742, PT. 1
Report Number: NASA-CR-62257
Accession Number
65N21775
Funding Number(s)
CONTRACT_GRANT: NAS8-11542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WEIGHT
SHELL
PRESSURE EFFECT
BUCKLING

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